Feedback control design for smooth, near-minimum time rotational maneuvers of flexible spacecraft /

Bibliographic Details
Main Author: Byers, Robert Michael
Format: Thesis eBook
Language:English
Published: [Place of publication not identified] : [publisher not identified] ; 1987.
Subjects:
Online Access:Link to OAKTrust copy

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Call Number: 1987 Thesis B9925
Notes: Cushing Archival Copy (Library Use Only)
 
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1987 Thesis B9925 Available

Available Online

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Call Number: 1987 Thesis B9925
 
Call Number Status Get It
1987 Thesis B9925 Available